Compact Airborne Spectral Sensor (COMPASS)

Christopher G. Simi; Edwin M. Winter; Mary M. Williams; David C. Driscoll

doi:10.1117/12.437000

20 August 2001 Compact Airborne Spectral Sensor (COMPASS)

Christopher G. Simi, Edwin M. Winter, Mary M. Williams, David C. Driscoll

Proceedings Volume 4381, Algorithms for Multispectral, Hyperspectral, and Ultraspectral Imagery VII; (2001) https://doi.org/10.1117/12.437000
Event: Aerospace/Defense Sensing, Simulation, and Controls, 2001, Orlando, FL, United States

Abstract

The COMPACT Airborne Spectral Sensor (COMPASS) design is intended to demonstrate a new design concept for solar reflective hyper spectral systems for the Government. Capitalizing from recent focal plane developments, the COMPASS system utilizes a single FPA to cover the 0.4-2.35micrometers spectral region. This system also utilizes an Offner spectrometer design as well as an electron etched lithography curved grating technology pioneered by NASA/JPL. This paper also discusses the technical trades, which drove the design selection of COMPASS. When completed, the core COMPASS spectrometer design could be used in a large variety of configurations on a variety of aircraft.

Citation Download Citation

Christopher G. Simi, Edwin M. Winter, Mary M. Williams, and David C. Driscoll "Compact Airborne Spectral Sensor (COMPASS)", Proc. SPIE 4381, Algorithms for Multispectral, Hyperspectral, and Ultraspectral Imagery VII, (20 August 2001); https://doi.org/10.1117/12.437000

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